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Category > Applied Sciences Posted 20 Jun 2017 My Price 5.00

A nozzle is designed assuming reversible adiabatic flow with an exit Mach number of 2.8

A nozzle is designed assuming reversible adiabatic flow with an exit Mach number of 2.8 while flowing air with a stagnation pressure and temperature of 2 MPa and 150â—¦C, respectively. The mass flow rate is 5 kg/s, and k may be assumed to be 1.40 and constant. Determine the exit pressure, temperature and area, and the throat area.

 

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Alpha Geek
(8)
Status NEW Posted 20 Jun 2017 11:06 AM My Price 5.00

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